Explore: Scale Models
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AI-Generated Overview About “scale-models”:
Books Results
Source: The Open Library
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Search results from The Open Library
1Material Bernini
By Carolina Mangone, Evonne Levy and Allison Levy
“Material Bernini” Metadata:
- Title: Material Bernini
- Authors: Carolina MangoneEvonne LevyAllison Levy
- Language: English
- Number of Pages: Median: 248
- Publisher: Taylor & Francis Group
- Publish Date: 2016 - 2018
“Material Bernini” Subjects and Themes:
- Subjects: ➤ Sculpture, italy - Criticism and interpretation - Models (Clay, plaster, etc.) - Maquettes (Sculpture) - Architectural models - Scale models - Dummies (printed matter) - ART - Sculpture & Installation - Bozzetto - Künstlerisches Material - Tonmodell - Tonplastik - Werkstoff
Edition Identifiers:
- The Open Library ID: ➤ OL33651623M - OL33620055M - OL33772825M - OL34656230M - OL33639788M - OL28802115M
- Online Computer Library Center (OCLC) ID: 946887361 - 915159413
- Library of Congress Control Number (LCCN): 2015029386
- All ISBNs: ➤ 1317099478 - 9781317099482 - 9781315594286 - 1317099486 - 113835306X - 9781317099499 - 1315594285 - 1472459229 - 9781317099475 - 9781472459220 - 1317099494 - 9781138353060
Access and General Info:
- First Year Published: 2016
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Low-power ion thruster development status
By Michael J. Patterson
“Low-power ion thruster development status” Metadata:
- Title: ➤ Low-power ion thruster development status
- Author: Michael J. Patterson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1999
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Low-power ion thruster development status” Subjects and Themes:
- Subjects: ➤ Ion engines - Ion propulsion - Engine design - Xenon - Scale models - Fabrication - Design analysis
Edition Identifiers:
- The Open Library ID: OL17839048M - OL17131677M - OL18132874M - OL15542497M
- Online Computer Library Center (OCLC) ID: 41519815
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel
By P. S. Barna
“Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel” Metadata:
- Title: ➤ Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel
- Author: P. S. Barna
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995 - 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel” Subjects and Themes:
- Subjects: ➤ Acoustic ducts - Blowing - Diffusers - Flow visualization - Nozzle design - Pressure recovery - Scale models - Sound detecting and ranging - Sound waves - Three dimensional models - Velocity measurement - Wind tunnel models - Wind tunnel nozzles - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL17838013M - OL15504898M - OL15504897M - OL17838014M
- Online Computer Library Center (OCLC) ID: 40132872 - 40122403
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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4Acoustic treatment design scaling methods
By R. E. Kraft
“Acoustic treatment design scaling methods” Metadata:
- Title: ➤ Acoustic treatment design scaling methods
- Author: R. E. Kraft
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999 - 2003
- Publish Location: ➤ - Hanover, MD - [Springfield, Va - Hampton, Va
“Acoustic treatment design scaling methods” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - High frequencies - Mathematical models - Aircraft models - Scale models - Aircraft engines - Acoustic impedance - Frequency ranges - Aircraft noise - Noise prediction (Aircraft) - Impedance measurement - Acoustic properties
Edition Identifiers:
- The Open Library ID: OL17621421M - OL17722881M - OL15554930M - OL17584196M
- Online Computer Library Center (OCLC) ID: 54914469 - 42269573
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications
By David E. Hahne
“Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications” Metadata:
- Title: ➤ Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications
- Author: David E. Hahne
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: ➤ Hanover, MD - Springfield, VA - Hampton, Va
“Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications” Subjects and Themes:
- Subjects: Databases - Leading edges - Scale models
Edition Identifiers:
- The Open Library ID: OL17594999M - OL15568015M - OL18139938M - OL18295719M
- Online Computer Library Center (OCLC) ID: 44121256
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter
By Arthur E. Phelps
“Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter” Metadata:
- Title: ➤ Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter
- Author: Arthur E. Phelps
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1985
- Publish Location: ➤ Springfield, Va - [Washington, D.C.]
“Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter” Subjects and Themes:
- Subjects: ➤ Military helicopters - Helicopter performance - Wind tunnel tests - Scale models - Aerodynamic characteristics - Stability - Testing - P-531 helicopter
Edition Identifiers:
- The Open Library ID: OL16115009M - OL18217713M - OL18468562M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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7Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model
By Stacey J. Cotton
“Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model” Metadata:
- Title: ➤ Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model
- Author: Stacey J. Cotton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Angle of attack - Buffeting - Flight tests - Flow visualization - Liquid-vapor interfaces - Scale models - Sideslip - Stabilizers (Fluid dynamics) - Tail assemblies - Vortices - Water tunnel tests - X-29 aircraft
Edition Identifiers:
- The Open Library ID: OL17001977M - OL17682958M - OL18076527M
- Online Computer Library Center (OCLC) ID: 32298726
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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8Crashworthy evaluation of a 1/5-scale model composite fuselage concept
By Karen E. Jackson
“Crashworthy evaluation of a 1/5-scale model composite fuselage concept” Metadata:
- Title: ➤ Crashworthy evaluation of a 1/5-scale model composite fuselage concept
- Author: Karen E. Jackson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: [Springfield, Va - Hampton, Va
“Crashworthy evaluation of a 1/5-scale model composite fuselage concept” Subjects and Themes:
- Subjects: ➤ Applications programs (Computers) - Composite materials - Crashes - Crashworthiness - Drop tests - Finite element method - Fuselages - Impact tests - Scale models - Structural reliability
Edition Identifiers:
- The Open Library ID: OL17135402M - OL17701300M - OL17591912M
- Online Computer Library Center (OCLC) ID: 42758525
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Micromechanical modeling of woven metal matrix composites
By Brett A. Bednarcyk
“Micromechanical modeling of woven metal matrix composites” Metadata:
- Title: ➤ Micromechanical modeling of woven metal matrix composites
- Author: Brett A. Bednarcyk
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Micromechanical modeling of woven metal matrix composites” Subjects and Themes:
- Subjects: ➤ Copper - Micromechanics - Thermal conductivity - Mathematical models - Scale models - Woven composites - Microstructure - Carbon - Metal matrix composites
Edition Identifiers:
- The Open Library ID: OL17124394M - OL17831291M - OL17696902M
- Online Computer Library Center (OCLC) ID: 39460405
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10Effects of eddy viscosity on time correlations in large eddy simulation
By He, Guowei.
“Effects of eddy viscosity on time correlations in large eddy simulation” Metadata:
- Title: ➤ Effects of eddy viscosity on time correlations in large eddy simulation
- Author: He, Guowei.
- Language: English
- Publisher: ➤ ICASE, NASA Langley Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2001
- Publish Location: Hanover, MD - Hampton, VA
“Effects of eddy viscosity on time correlations in large eddy simulation” Subjects and Themes:
- Subjects: ➤ Acoustic simulation - Direct numerical simulation - Eddy viscosity - Estimates - Large eddy simulation - Scale models - Viscous drag
Edition Identifiers:
- The Open Library ID: OL17607396M - OL16031846M
- Online Computer Library Center (OCLC) ID: 50060785
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11The Modelmaker's Handbook
By Albert Jackson and David Day
“The Modelmaker's Handbook” Metadata:
- Title: The Modelmaker's Handbook
- Authors: Albert JacksonDavid Day
- Language: English
- Number of Pages: Median: 352
- Publisher: Dorling Kindersley
- Publish Date: 1981
- Publish Location: London, England
“The Modelmaker's Handbook” Subjects and Themes:
- Subjects: ➤ Modelling - airplane models - scale models - model making - dioramas - Models and modelmaking
Edition Identifiers:
- The Open Library ID: OL24869413M
- Library of Congress Control Number (LCCN): 80002702
- All ISBNs: 9780394507880 - 0394507886
Author's Alternative Names:
"Day, David, 1947-"Access and General Info:
- First Year Published: 1981
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12A reduced model for prediction of thermal and rotational effects on turbine tip clearance
By Javier A. Kypuros
“A reduced model for prediction of thermal and rotational effects on turbine tip clearance” Metadata:
- Title: ➤ A reduced model for prediction of thermal and rotational effects on turbine tip clearance
- Author: Javier A. Kypuros
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2003
- Publish Location: [Cleveland, Ohio]
“A reduced model for prediction of thermal and rotational effects on turbine tip clearance” Subjects and Themes:
- Subjects: ➤ Blade tips - Clearances - Dynamic models - Mathematical models - Scale models - Temperature effects - Turbine blades
Edition Identifiers:
- The Open Library ID: OL17722590M - OL17635033M
- Online Computer Library Center (OCLC) ID: 58833954
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Atmospheric probe model
By Jerald M. Vogel
“Atmospheric probe model” Metadata:
- Title: Atmospheric probe model
- Author: Jerald M. Vogel
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Atmospheric probe model” Subjects and Themes:
- Subjects: ➤ Pressure distribution - Probes - Ring wings - Scale models - Velocity distribution - Wind tunnel models - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17595599M - OL15546934M
- Online Computer Library Center (OCLC) ID: 42695835
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring
By Steven A. Johnson
“A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring” Metadata:
- Title: ➤ A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring
- Author: Steven A. Johnson
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ Springfield, Va - [Washington, D.C.]
“A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring” Subjects and Themes:
- Subjects: ➤ Airplanes - Computer simulation - Dynamic models - F-18 aircraft - Motors - Real time operation - Real-time data processing - Scale models - Thrust - Thrust distribution - Thrust vector control - Turbofan engines
Edition Identifiers:
- The Open Library ID: OL16132236M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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15Aerodynamic simulation of ice accretion on airfoils
By Andy P. Broeren
“Aerodynamic simulation of ice accretion on airfoils” Metadata:
- Title: ➤ Aerodynamic simulation of ice accretion on airfoils
- Author: Andy P. Broeren
- Language: English
- Number of Pages: Median: 66
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2011
- Publish Location: Cleveland, Ohio
“Aerodynamic simulation of ice accretion on airfoils” Subjects and Themes:
- Subjects: ➤ Airfoils - Ice formation - Wind tunnel tests - Aerodynamic stalling - Scale models - Simulation
Edition Identifiers:
- The Open Library ID: OL43888753M
- Online Computer Library Center (OCLC) ID: 769137623
Access and General Info:
- First Year Published: 2011
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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16Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A
By James H. Dittmar
“Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A” Metadata:
- Title: ➤ Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A
- Author: James H. Dittmar
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1985
- Publish Location: [Cleveland, Ohio
“Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A” Subjects and Themes:
- Subjects: ➤ Airplanes - Design analysis - Evaluation - Helical flow - Mach number - Measurement - Noise - Noise (Sound) - Noise reduction - Predictions - Prop-fan technology - Propeller blades - Scale models - Supersonic speed - Tip speed - Turbine-propeller engines - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL16151292M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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17Design and fabrication of the NASA HL-20 full scale research model
By K. Dean Driver
“Design and fabrication of the NASA HL-20 full scale research model” Metadata:
- Title: ➤ Design and fabrication of the NASA HL-20 full scale research model
- Author: K. Dean Driver
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center? - North Carolina State University, Mechnical and Aerospace Engineering, Mars Mission Research Center
- Publish Date: 1991
- Publish Location: Raleigh, NC - [Hampton, VA
“Design and fabrication of the NASA HL-20 full scale research model” Subjects and Themes:
- Subjects: ➤ Space transportation system - Launch vehicles - Spacecrews - Spacecraft design - Scale models - Fabrication
Edition Identifiers:
- The Open Library ID: OL18263324M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18Analysis of advanced solid rocket motor ignition phenomena
By Winfred A. Foster
“Analysis of advanced solid rocket motor ignition phenomena” Metadata:
- Title: ➤ Analysis of advanced solid rocket motor ignition phenomena
- Author: Winfred A. Foster
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Analysis of advanced solid rocket motor ignition phenomena” Subjects and Themes:
- Subjects: ➤ Solid propellant rocket engines - Pressure distribution - Heat transfer coefficients - Wind tunnel tests - Scale models - Propulsion system performance - Advanced solid rocket motor (STS) - Flow distribution - Ignition - Space shuttle boosters
Edition Identifiers:
- The Open Library ID: OL15418933M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Analysis of wind tunnel oscillatory data of the X-31A aircraft
By Mark S. Smith
“Analysis of wind tunnel oscillatory data of the X-31A aircraft” Metadata:
- Title: ➤ Analysis of wind tunnel oscillatory data of the X-31A aircraft
- Author: Mark S. Smith
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - Springfield, VA
“Analysis of wind tunnel oscillatory data of the X-31A aircraft” Subjects and Themes:
- Subjects: ➤ X-31 aircraft - Unsteady aerodynamics - Mathematical models - Wind tunnel tests - Static stability - Scale models - Dynamic stability - Harmonic oscillation - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL15542620M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Turbulent inflow measurements
By Albert R. George
“Turbulent inflow measurements” Metadata:
- Title: Turbulent inflow measurements
- Author: Albert R. George
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Turbulent inflow measurements” Subjects and Themes:
- Subjects: ➤ Acoustic measurement - Flow measurement - Aerodynamic characteristics - Scale models - Tilt rotor aircraft - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15487174M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Performance of a miniaturized arcjet
By John M. Sankovic
“Performance of a miniaturized arcjet” Metadata:
- Title: ➤ Performance of a miniaturized arcjet
- Author: John M. Sankovic
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Performance of a miniaturized arcjet” Subjects and Themes:
- Subjects: ➤ Viscous flow - Engine design - Anodes - Scale models - Breadboard models - Propulsion system performance - Engine tests - Electric propulsion - Spacecraft power supplies - Arc jet engines
Edition Identifiers:
- The Open Library ID: OL15420843M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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22Design and checkout of a high speed research nozzle evaluation rig
By Raymond S. Castner
“Design and checkout of a high speed research nozzle evaluation rig” Metadata:
- Title: ➤ Design and checkout of a high speed research nozzle evaluation rig
- Author: Raymond S. Castner
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1997
- Publish Location: ➤ Springfield, VA - [Cleveland, Ohio]
“Design and checkout of a high speed research nozzle evaluation rig” Subjects and Themes:
- Subjects: Evaluation - Design analysis - Scale models - High speed - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL15543119M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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23Comparison of the aerodynamic characteristics of similar models in two size wind tunnels at transonic speeds
By A. M. Springer
“Comparison of the aerodynamic characteristics of similar models in two size wind tunnels at transonic speeds” Metadata:
- Title: ➤ Comparison of the aerodynamic characteristics of similar models in two size wind tunnels at transonic speeds
- Author: A. M. Springer
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Comparison of the aerodynamic characteristics of similar models in two size wind tunnels at transonic speeds” Subjects and Themes:
- Subjects: Wind tunnel models - Transonic speed - Scale models - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL15546876M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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24Development of the CSI phase-3 evolutionary model testbed
By M. J. Gronet
“Development of the CSI phase-3 evolutionary model testbed” Metadata:
- Title: ➤ Development of the CSI phase-3 evolutionary model testbed
- Author: M. J. Gronet
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Development of the CSI phase-3 evolutionary model testbed” Subjects and Themes:
- Subjects: ➤ Dynamic response - Earth Observing System (EOS) - Ground tests - Modal response - Scale models - Space environment simulation - Spacecraft models - Test stands
Edition Identifiers:
- The Open Library ID: OL15402729M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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25Preliminary design, analysis, and costing of a dynamic model of the NASA space station
By M. J. Gronet
“Preliminary design, analysis, and costing of a dynamic model of the NASA space station” Metadata:
- Title: ➤ Preliminary design, analysis, and costing of a dynamic model of the NASA space station
- Author: M. J. Gronet
- Number of Pages: Median: 203
- Publisher: Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va
“Preliminary design, analysis, and costing of a dynamic model of the NASA space station” Subjects and Themes:
- Subjects: Dynamic tests - Space stations - Scale models
Edition Identifiers:
- The Open Library ID: OL19003272M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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26Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances
By Lisa J. Bjarke
“Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances” Metadata:
- Title: ➤ Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances
- Author: Lisa J. Bjarke
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Facility
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances” Subjects and Themes:
- Subjects: ➤ Wing camber - Flow visualization - Flutter analysis - Buffeting - Aeroelasticity - Scale models - Flight tests
Edition Identifiers:
- The Open Library ID: OL16123834M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27Methods for scaling icing test conditions
By David N. Anderson
“Methods for scaling icing test conditions” Metadata:
- Title: ➤ Methods for scaling icing test conditions
- Author: David N. Anderson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Methods for scaling icing test conditions” Subjects and Themes:
- Subjects: Aircraft icing - Scaling laws - Scale models - Scale effect - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15411126M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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28Testing of densified liquid hydrogen stratification in a scale model propellant tank
By John M. Jurns
“Testing of densified liquid hydrogen stratification in a scale model propellant tank” Metadata:
- Title: ➤ Testing of densified liquid hydrogen stratification in a scale model propellant tank
- Author: John M. Jurns
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for AeroSpace Information
- Publish Date: 2001
- Publish Location: Hanover MD - Cleveland, Ohio
“Testing of densified liquid hydrogen stratification in a scale model propellant tank” Subjects and Themes:
- Subjects: ➤ Performance tests - Propellant tanks - Cryogenic fluid storage - Stratification - Liquid hydrogen - Scale models
Edition Identifiers:
- The Open Library ID: OL16036982M
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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29Experimental studies in helicopter vertical climb performance
By R. M. McKillip
“Experimental studies in helicopter vertical climb performance” Metadata:
- Title: ➤ Experimental studies in helicopter vertical climb performance
- Author: R. M. McKillip
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Experimental studies in helicopter vertical climb performance” Subjects and Themes:
- Subjects: ➤ Performance tests - Climbing flight - Flow visualization - Helicopter performance - Scale models - Numerical analysis
Edition Identifiers:
- The Open Library ID: OL15540248M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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30Lobed mixer design for noise suppression
By Vinod Govind Mengle
“Lobed mixer design for noise suppression” Metadata:
- Title: ➤ Lobed mixer design for noise suppression
- Author: Vinod Govind Mengle
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2002
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA
“Lobed mixer design for noise suppression” Subjects and Themes:
- Subjects: ➤ Acoustic properties - Aerodynamic characteristics - Aerodynamic noise - Aircraft noise - Data bases - Databases - Jet flow - Noise reduction - Scale models - Velocity
Edition Identifiers:
- The Open Library ID: OL16139153M
Access and General Info:
- First Year Published: 2002
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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31Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air
By William I. Scallion
“Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air” Metadata:
- Title: ➤ Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air
- Author: William I. Scallion
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air” Subjects and Themes:
- Subjects: ➤ Controllability - Effectiveness - Wind tunnel tests - Scale models - Aerodynamic characteristics - Lifting bodies - Elevons - Fins
Edition Identifiers:
- The Open Library ID: OL18139203M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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32RSRM 10% Scale Model drilled hole plate tests
“RSRM 10% Scale Model drilled hole plate tests” Metadata:
- Title: ➤ RSRM 10% Scale Model drilled hole plate tests
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - The Operation
- Publish Date: 1996
- Publish Location: ➤ Huntsville, AL - Springfield, Va - [Washington, DC
“RSRM 10% Scale Model drilled hole plate tests” Subjects and Themes:
- Subjects: ➤ Combustion - Perforated plates - Scale models - Burning time - Discharge coefficient - Flow distribution - Mass flow rate - Performance prediction - Holes (Mechanics)
Edition Identifiers:
- The Open Library ID: OL17827047M
- Online Computer Library Center (OCLC) ID: 39204162
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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